FIELD: transportation.
SUBSTANCE: system contains fuel level sensors (3) installed in fuel tank and magnetically operated float fuel level switches (4) as well as the first and the second fuel volume measurement units (6 and 7), fuel mass calculating unit (5) and instrument for determination of fuel surface spatial position (10), fuel density measurement unit (9), fuel density comparator (8). Additionally, the system includes multisensor (2) of fuel characteristic parametres installed in fuel tank which multisensor contains dielectric permeability sensor (14) and sensor of ultrasound speed (15) in fuel. Fuel level sensor represents electric-capacity level sensor structurally combined with ultrasonic level sensor. Electric-capacity level sensor is made as coaxial cylindrical condenser with internal and external electrodes and fuel level ultrasonic sensor is made as tubular acoustic waveguide. Float acoustic reflector with constant magnet installed in it is used as float of magnetically operated float fuel level switch.
EFFECT: decrease in fuel mass measurement error.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
ON-BOARD AIRCRAFT FUEL MEASUREMENT SYSTEM | 2008 |
|
RU2384482C1 |
FUEL MEASUREMENT SYSTEM FOR AIRCRAFT | 2008 |
|
RU2382724C1 |
ON-BOARD FUEL MEASUREMENT SYSTEM | 2008 |
|
RU2384481C1 |
ON-BOARD FUEL-MEASURING ELECTRIC-CAPACITY SYSTEM OF AIRPLANE | 2008 |
|
RU2382727C1 |
ON-BOARD FUEL CAPACITIVE MEASUREMENT SYSTEM | 2008 |
|
RU2384486C1 |
ON-BOARD AIRCRAFT FUEL MEASUREMENT SYSTEM | 2008 |
|
RU2384483C1 |
ON-BOARD AIRCRAFT FUEL MEASUREMENT SYSTEM | 2008 |
|
RU2384485C1 |
FUEL MEASUREMENT CAPACITIVE SYSTEM | 2008 |
|
RU2384484C1 |
FUEL MEASUREMENT ELECTRIC-CAPACITY SYSTEM FOR AIRCRAFT | 2008 |
|
RU2382726C1 |
FUEL-MEASURING ELECTRIC-CAPACITY SYSTEM OF AIRPLANE | 2008 |
|
RU2382723C1 |
Authors
Dates
2010-02-27—Published
2008-07-15—Filed